NUTS, SELF-LOCKING, NICKEL ALLOY, UNS N07001 180 000 psi, ALL METAL 1400 °F USE, UNJ THREAD FORM
- Aerospace Standard
|Aerospace Material Specification||Iron Alloy, Corrosion and Heat Resistant, Covered, Welding Electrodes 31Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0 (Cb + Ta)|
|Aerospace Material Specification||Tantalum Sheet, Strip, and Plate Annealed|
Data Sets - Support Documents
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.